US6073011A - Communication satellite load balancing system and method - Google Patents
Communication satellite load balancing system and method Download PDFInfo
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- US6073011A US6073011A US08/575,741 US57574195A US6073011A US 6073011 A US6073011 A US 6073011A US 57574195 A US57574195 A US 57574195A US 6073011 A US6073011 A US 6073011A
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/1853—Satellite systems for providing telephony service to a mobile station, i.e. mobile satellite service
- H04B7/18539—Arrangements for managing radio, resources, i.e. for establishing or releasing a connection
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- the present invention relates generally to communication satellites. More particularly, the present invention relates to a satellite load balancing system and method which maximize the regional system capacity for a multiplicity of satellites and users.
- telecommunication satellites have generally been positioned in a particular geostationary orbit to serve a fixed geographic area. More recently, medium-earth-orbit communication satellite systems and low-earth-orbit communication satellite systems have been proposed for global telecommunication. Such lower altitude satellite configurations permit the communication satellites to service different geographical regions over time since the satellites would not be essentially fixed over a geographical point of the earth. The geographical regions to which communication satellite systems provide communication transmissions are designated as service regions.
- a lower altitude communication satellite configuration may be capable of two or more of its communication satellites supporting the same service region.
- the degree of communication satellite depends on its current position relative to the service region.
- the overall lower altitude communication satellite regional system capacity varies with time because of the satellite motion, and also with the geographic subscriber distribution.
- the traditional communication satellite capacity definition does not focus on the level of service that an entire system of satellites can provide to a given service region.
- a method of controlling system capacity in a satellite-based cellular telecommunication system involves a plurality of communication satellites orbiting above a commonly-covered region of the earth and a plurality of mobile cellular stations which are capable of communicating with at least a plurality of said orbiting communication satellites during at least some interval of time.
- the method includes the step of determining, for each of the communication satellites at periodic intervals, a power utilization factor which is selectively employed to avoid a communication saturation condition for any of the communication satellites.
- the method also includes the step of assigning a communication channel between the mobile cellular station and one of the orbiting satellites on the basis of a criterion that includes the power utilization factor.
- a mobile cellular station is enabled to override the assignment in response to environmental conditions, such that a different communication channel between the mobile cellular station and one of said orbiting satellites will be determined by the mobile cellular station.
- the assignment is uploaded from an earth-based station to the communication satellites.
- the uploaded assignment is broadcast from each of the communication satellites to the commonly-covered region.
- the power utilization factor is employed when the communication channel load on one of the communication satellites exceeds a predetermined amount.
- Another feature of the invention includes the power utilization factor minimizing the maximum single-satellite power required for said communication satellites to supply a predetermined number of communication channels in accordance with the geographic distribution of demand.
- Another feature of the invention includes the power utilization factor leveling the communication channel load between communication satellites.
- the present invention can be applied to a system of lower-altitude communication satellites for mobile cellular communications.
- a mobile cellular station can communicate to a control station and to its ultimate destination through one of the communication satellites that has been assigned to the mobile cellular station by the control station.
- FIG. 1 is a schematic illustration of a satellite based cellular telecommunications system which may be utilized in accordance with the present invention
- FIG. 2 is a schematic illustration of a constellation of telecommunication satellites providing single global land mass coverage of the earth;
- FIG. 3 is a schematic illustration of a constellation of telecommunication satellites providing double global land mass coverage of the earth
- FIG. 4 is a schematic illustration of a constellation of telecommunication satellites providing single hemispheric coverage of the earth
- FIG. 5 is a schematic illustration of a constellation of telecommunication satellites providing double hemispheric coverage of the earth
- FIG. 6 is a schematic illustration of a original constellation of telecommunication satellites which provides partial coverage of the earth
- FIG. 7 is a schematic illustration can follow-on constellation of telecommunication satellites which provides further coverage of the earth;
- FIG. 8 is a schematic illustration of a full baseline constellation of telecommunication satellites which provides complete land mass coverage of the earth
- FIG. 9 is a cartographic illustration of satellite visibility using the original constellation of FIG. 6;
- FIG. 10 is a graphical illustration of satellite coverage using the original constellation of FIG. 6;
- FIG. 11 is another graphical illustration of satellite coverage using the original constellation of FIG. 6;
- FIGS. 12A-12E provide a cartographic illustration of satellite coverage using the original constellation of FIG. 6;
- FIGS. 13A-13G provide a cartographic illustration of the variable antenna pattern using a beam-steering method
- FIG. 14 is a cartographic illustration of satellite visibility using an alternate constellation wherein each of the satellites reside in their own individual orbital planes;
- FIG. 15 is a graphical illustration of satellite coverage using the original constellation referred to in FIG. 14;
- FIG. 16 is another graphical illustration of satellite coverage using the original constellation referred to in FIG. 14;
- FIG. 17 is a flow chart which illustrates a coordinated boresight steering method
- FIG. 18 is a schematic block diagram of a satellite-based mobile communication system incorporating a mobile handset tracking and paging system which may be utilized in accordance with the present invention
- FIGS. 19a, 19b, 19c and 19d illustrate a grid including a plurality of grid sections, fixed with respect to the earth, and a plurality of individual focused beams generated by one or more sub-geosynchronous satellites;
- FIG. 20 is a schematic block diagram of a mobile handset
- FIG. 21 is a flowchart of a registration operation performed by the mobile handset tracking and paging system
- FIG. 22 provides a cartographic exemplary illustration of overlapping satellite coverage and grid divisions of a service region
- FIG. 23 is a flowchart which illustrates functional interactions among a control station, a communication satellite, and a mobile cellular station for performing the operations of the present invention
- FIGS. 24A and 24B provide a flowchart which illustrates the communication satellite load balancing method for achieving maximum regional system capacity
- FIG. 25 is a graph which shows the satellite system capacity for a service region over time when the communication satellites are selected by mobile cellular stations.
- FIG. 26 is a graph which shows the satellite system capacity for a service region over time when the communication satellites are assigned by a control station.
- communication satellite 301, communication satellite 302, and communication satellite 303 are capable of providing bi-directional communication services for a service region 310 which contains a plurality of mobile cellular stations.
- the communication satellites handle the communications for the mobile cellular stations within the service region 310.
- the United States was chosen as the service region 310.
- other communication satellites will be providing communication services at the same time to other regions around the world, such as Europe, Asia and South America.
- the system could be designed with the world representing a single region and with the power balanced among all of the system satellites.
- the service region 310 is divided up into grids located at 312.
- the size of these grids are preferably small enough so that a communication satellite appears at approximately the same elevation angle to mobile cellular stations within the same grid.
- the grids are rectangular and have the dimensions of 2 degrees by 2 degrees. It should be understood that many other grid sizes and grid shapes are within the scope of the present invention.
- Within the squared set of grids generally designated by reference numeral 312 are a varying number of mobile cellular stations.
- Communication satellite 301 provides a first area of coverage 321 for a portion of the service region 310.
- Communication satellite 302 provides a second area of coverage 322 for a portion of the service region 310 and communication satellite 303 provides a third area of coverage 323 for a portion of the service region 310.
- the three areas of coverage partially overlap one another.
- the overlapping coverage area which is the commonly-covered service region of the three communication satellites is depicted as the area enclosed by curve 331, curve 332, and curve 333. Also grid 340, grid 342, grid 344, and grid 346 are contained within the overlapping coverage area.
- a power utilization factor is determined as necessary to provide a down-link of fixed bandwidth transmission to each of the covered grids.
- the radio frequency (RF) power required for a single-satellite transmission is determined for each of the commonly covered grids.
- the RF power required for a down-link transmission by communication satellite 301 to grid 340 would be determined.
- the RF power required for a transmission by the other two communication satellites to grid 340 would be determined.
- one of the communication satellites 301-303 After completing the determination of the RF power required for a transmission of each communication satellite to all of the covered grids, one of the communication satellites 301-303 would be assigned to a commonly covered grid based on the determined values of the power utilization factor. More particularly, a set of assignments is preferably made that minimizes the maximum RF power required of any satellite for the communication satellite system to supply a single transmission to each of the region's grids.
- the present invention includes at least one control station 350 to assist in assigning communications from the three communication satellites to the commonly covered grids. It should be appreciated that more than one control station may be used and placed in locations other than the exemplary location of the control station 350 in FIG. 22.
- FIG. 23 shows the present invention's functional interactions among the control station, communication satellites, and mobile cellular stations.
- the start indicator 400 indicates that the control station function at block 402 is processed first.
- Block 402 designates that the control station assigns communication satellites to mobile cellular stations.
- block 404 depicts that the control station uploads the assignments to the communication satellites.
- a mobile cellular station may request a satellite assignment other than the one selected by the control station. For example, a mobile cellular station may request to use a different communication satellite when the mobile cellular station is not able to establish a sufficiently reliable communication link with the particular communication satellite that was assigned by the control station. Such a situation could arise when the mobile cellular station is at least partially blocked from the assigned communication satellite by buildings.
- the flow for this aspect of the present invention proceeds to the exit indicator 420.
- the mobile cellular station will initiate communication through the pre-assigned satellite when the user desires to place a telephone call or otherwise begin an appropriate communication session (such as voice, data, video and so forth) with another communication station.
- the mobile cellular station also listens to the pre-assigned satellite for an incoming call while in standby mode.
- the flow for this aspect of the invention continues at block 410.
- the mobile cellular station uploads the requested satellite assignment to the pre-assigned communications satellite.
- the pre-assigned communication satellite downloads the requested assignment to the control station.
- the control station processes that requested assignment at block 414 where the control station assigns the requested satellite to the mobile cellular station. Thereupon, the flow for this aspect of the invention proceeds to the exit indicator 420.
- the present invention is concerned with power-limited applications.
- the assignment method according to the present invention may need to be modified to accommodate other such concerns.
- time limitations due to the time varying nature of coverage provided by a non-geostationary satellite, there may be time limitations as well as bandwidth limitations.
- the most appropriate assignment criteria in a given situation may be based upon the time remaining for a satellite to cover an area, as set forth above. Accordingly, it should be understood that the assignment criteria may be dependent upon several competing factors, and that the power utilization factor taught herein is an important factor since it may be employed according to the present invention to maximize regional capacity.
- the present invention may be employed in satellite-based cellular telecommunication systems that employ satellites in both low and medium-earth altitude orbits. While the present invention is particularly effective in the medium-earth altitude systems described above, the present invention has applicability to any satellite-based cellular telecommunication systems which have satellites in non-geostationary orbits where two or more satellites are capable of simultaneously covering the same cellular region. For example, a number of low-earth altitude cellular telecommunication systems have been proposed (that is, satellite-based systems whose orbits are disposed below the Van Allen Belts). These systems also provide a degree of multiple satellite coverage.
- control station 350 it is preferred that control station upload assignment information to the satellites as they pass overhead for a predetermined period of time. For example, in the situation where a satellite, such as satellite 303, passes over control station 350 once per day, then the control station may upload all of the assignment information needed by the satellite 303 for a period of at least one day. However, this is not to say that the uploaded assignment information may not be for suitably longer periods of time, because it may be more appropriate to upload such information for longer periods of time, such as a week. Aside from the need to periodically upload assignment instructions to a satellite, it should be understood that the present invention does not depend upon the number of orbits employed or other similar constellation building specifications. Indeed, even the control stations themselves do not need to be fixed ground stations per se, as airborne or maritime control stations could be employed as well.
- the control station(s) will preferably employ historical data of power utilization requirements in the past in order to determine the most appropriate assignments for the satellites in the next service period.
- FIG. 24a illustrates the preferred communication satellite transmission load balancing method and apparatus in greater detail.
- the start indicator 450 indicates that the initial step at block 452 is processed first.
- Block 452 depicts that the grid division identification data for a desired service region is retrieved from the database.
- Block 456 an iterative construct w designates that the next several blocks of the flowchart are to be performed for each satellite which has a field of view of the desired service region. Within the iterative construct of block 456 is block 458. Block 458 is another iterative construct which designates that the next several blocks are to be performed for each of grid.
- the decision block 460 is processed which inquires whether the grid for the particular iteration of block 458 is within the field of view of the current communication satellite for the particular iteration of block 456. If the grid is not within the field of view of the current communication satellite, then processing continues at block 464. However, if the grid is within the field of view, then at block 462 the satellite's RF power required to supply a single channel to the selected grid for the current iteration of block 456 is calculated.
- Block 464 inquires whether all of the grids have been evaluated for the communication satellite of the current iteration of block 456. If more grids need to be evaluated, then processing resumes at block 458 which allows the next grid to be evaluated for the communication satellite of the current iteration of block 456. However if no more grids need to be evaluated for the communication satellite of the current iteration of block 456, then processing continues at block 468.
- Block 468 inquires whether all of the communication satellites that have a field of view of the desired service region have been processed. If additional communication satellites need to be evaluated, then processing resumes at block 456 which allows the next selected communication satellite to be evaluated. However if additional communication satellites are not to be evaluated, then the flow branches to the flowchart "A" continuation indicator 470.
- FIG. 24b continues the processing from the flowchart "A" continuation indicator 470 at block 472.
- Block 472 states the underlying premise which is valid for the remainder of the flowchart that a region of "N" grids is covered by "S” satellites.
- Block 474 is an iterative construct which designates that the next several blocks are to be performed for each possible assignment of "N" grids to "S" satellites. Within the iterative construct of block 474 is block 476. For each satellite, block 476 computes the RF power required to support a single carrier to each grid assigned to it. Block 478 then identifies the satellite with the maximum RF power requirement.
- the decision block 480 inquires if the maximum RF power is less than the smallest maximum RF power found for previous grid assignments. If it not less, then processing continues at decision block 484. However if the maximum RF power is less than the smallest maximum RF power found for previous grid assignments, then block 482 replaces the old minimax RF power with the new minimax RF power. Thereupon processing continues at decision block 484.
- Decision b k 484 inquires if the grid assignment loop has completed. If the loop has not completed, then processing returns to block 474 for the next iteration of the grid assignment loop. If the loop has completed, then processing terminates at the stop indicator 486.
- the methodology of FIG. 24B requires that the control station considers every possible assignment of "N" grids to "S" satellites. However, such a large comparison need not necessarily be conducted. According to the process of FIG. 24B, S N possible sets of assignments must be considered. For certain values of "S" and "N", the set S N may be unduly large. Therefore, it may be desirable to substitute an alternative method, for that of FIG. 24B, which examines a subset of the total number of possible sets of assignments S N . The alternative methods may vary so long as they provide the optimum set of assignments or one that affords a system capacity nearly as large as the capacity associated with the optimum assignment set.
- Ps is the RF power available from each communication satellite
- Pm is the minimax communication satellite power
- N is the number of selected grids.
- each grid contains an entry which is proportional to the user density in the grid.
- the entries might range from 1 to 10.
- there "G” grids and the entry in the "ith" grid is denoted by “n i ".
- the communication satellite RF power required to supply grid "i" with "n” channels is computed for each communication satellite that covers grid "i”.
- the set of assignments of communication satellites to grids is selected that minimizes the maximum single communication satellite RF power required for the communication satellites collectively to supply grid "i" with "n i " channels, for all values of i.
- the system capacity is:
- Ps is the RF power available from each satellite
- Pm' is the minimax satellite power
- N is determined by the following equation: ##EQU1##
- the present invention may use the environment type to modify the required communication satellite power per channel accordingly.
- the present invention may also allow a pair of communication satellites to share support of a grid. Depending on the number of grids involved in the optimization process, these refinements may yield a significant reduction in the minimax communication satellite power and accordingly will yield a significant increase in the computed communication satellite capacity for a service region.
- FIG. 25 and FIG. 26 illustrate the efficacy of the assignment method and system of the present invention.
- the service region chosen for this example was North America, periodically covered by various combinations of twelve communication satellites which is orbiting at an altitude of 5600 nautical miles.
- Data for the mobile cellular stations that comprise this service region were generated by representing the mobile cellular subscriber population by eighteen population centers spread across North America. Equal weight was given to each of the locations.
- the graph of FIG. 25 shows an exemplary communication satellite system capacity over a twenty-four hour period for the North American landmass.
- the ordinate axis shows the communication satellite system capacity in terms of channels available to the North American service region, under the condition that the satellites are selected independently by the mobile cellular station.
- FIG. 26 is a graph similar to the graph of FIG. 25. The distinction is that the graph of FIG. 26 shows the communication satellite system capacity where the communication satellites are assigned by the control station. A comparison of the two communication satellite system capacity profiles demonstrates that assignments by the control station results in a substantially higher communication satellite system transmission capacity.
- a reasonable way to measure communication satellite transmission capacity is the level of busy-hour offered traffic for which the blocking probability does not exceed X% more than Y% of the time.
- the system capacity in FIG. 25 is at most 2000 channels.
- the system capacity in FIG. 26, computed in the same manner exceeds 3000 channels.
- the communication satellite system transmission capacity for a service region may be increased by more than 50% by assigning communication satellites in conformity with the present invention.
- a reason for the substantially higher system capacity for the control station assignment approach is that if each mobile cellular station were allowed to communicate through a communication satellite of its own choosing, it typically would decide on the basis of its received signal strength. This mobile cellular station assignment approach could lead to one of the communication satellites becoming saturated while one or more of the other communication satellites remained unnecessarily underutilized.
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Abstract
Description
System Capacity (in channels)=(Ps/Pm)*N
System Capacity (in channels =(Ps/Pm')*N
Claims (11)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/575,741 US6073011A (en) | 1995-12-19 | 1995-12-19 | Communication satellite load balancing system and method |
TW085111980A TW333728B (en) | 1995-12-19 | 1996-10-01 | The satellite-based cellular telecommunication system & method for controlling system capacity |
CA002187008A CA2187008A1 (en) | 1995-12-19 | 1996-10-02 | Communication satellite load balancing system and method |
EP96116161A EP0780997A3 (en) | 1995-12-19 | 1996-10-09 | Communication satellite load balancing system and method |
JP27585796A JP3261320B2 (en) | 1995-12-19 | 1996-10-18 | Communication satellite load balancing system and method |
CN96119764A CN1157509A (en) | 1995-12-19 | 1996-12-10 | Communication satellite load balancing system and method |
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US08/575,741 US6073011A (en) | 1995-12-19 | 1995-12-19 | Communication satellite load balancing system and method |
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US6073011A true US6073011A (en) | 2000-06-06 |
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US08/575,741 Expired - Lifetime US6073011A (en) | 1995-12-19 | 1995-12-19 | Communication satellite load balancing system and method |
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EP (1) | EP0780997A3 (en) |
JP (1) | JP3261320B2 (en) |
CN (1) | CN1157509A (en) |
CA (1) | CA2187008A1 (en) |
TW (1) | TW333728B (en) |
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US7177649B1 (en) * | 1999-05-20 | 2007-02-13 | Avaya Technology Corp. | System for load balancing based on class of service for wireless communication networks |
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US7369809B1 (en) | 2000-10-30 | 2008-05-06 | The Directv Group, Inc. | System and method for continuous broadcast service from non-geostationary orbits |
US20090051588A1 (en) * | 2005-09-23 | 2009-02-26 | Thales | Device for transmitting and/or receiving signals with frequency re-use by assignment of a cell for each terminal, for a communication satellite |
US20090270088A1 (en) * | 2008-04-28 | 2009-10-29 | Eutelsat | Telecommunication network |
US11259212B2 (en) * | 2017-12-15 | 2022-02-22 | Gogo Business Aviation Llc | Dynamic load balancing of satellite beams |
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EP0935351A1 (en) * | 1998-01-29 | 1999-08-11 | ICO Services Ltd. | Radio resource management in a mobile satellite telephone system |
EP0978955A1 (en) * | 1998-08-04 | 2000-02-09 | ICO Services Ltd. | Zonal congestion control in a mobile satellite communication system |
EP0978954A1 (en) * | 1998-08-04 | 2000-02-09 | ICO Services Ltd. | LEO mobile satellite communication system with congestion control |
US6522636B1 (en) * | 1999-10-01 | 2003-02-18 | Motorola, Inc. | Satellite communications system and method with real-time power-based flow control |
US8023489B2 (en) * | 2004-03-17 | 2011-09-20 | Qualcomm, Inc. | Burden sharing in satellite communications |
EP2074849B1 (en) | 2006-09-26 | 2019-05-01 | QUALCOMM Incorporated | Sensor networks based on wireless devices |
CN111629400B (en) * | 2019-02-27 | 2022-03-29 | 华为技术有限公司 | Method, device and system for satellite cooperative communication |
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Also Published As
Publication number | Publication date |
---|---|
JPH09181668A (en) | 1997-07-11 |
EP0780997A2 (en) | 1997-06-25 |
CN1157509A (en) | 1997-08-20 |
JP3261320B2 (en) | 2002-02-25 |
EP0780997A3 (en) | 2001-09-05 |
CA2187008A1 (en) | 1997-06-20 |
TW333728B (en) | 1998-06-11 |
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